Abstract:
An apparatus having a smart material actuator, a support structure and at least one temperature compensating material insert, either externally mounted to the support structure, integrally formed with the support structure, or any combination thereof. The apparatus includes a mechanically leveraged electrically stimulated smart material. The support structure and actuator are susceptible to the effects of differences in thermal coefficients of expansion of the materials used in the construction. The smart material typically displaces less than 0.001 inches and is leveraged up to fifty times to obtain useful movement. The temperature effect on the smart material is therefore leveraged and amplified producing undesirable motion in the apparatus with ambient and/or operating temperature changes. A method for dimensioning and placement of a compensating insert with respect to the support structure provides an accurate and cost effective compensating insert.
Abstract:
A thermal microactuator is provided that can be deflected in multiple positions. The actuator has a hot arm and a cold arm coupled together at their distal ends suspended above a reference plane of a substrate. A potential difference is applied across the hot arm so that a current circulates through the hot arm but not the cold arm.
Abstract:
A drive mechanism for use in the transmission of power from a plurality of linear reciprocating power generating elements to a rotating output element. The drive mechanism includes a drive cam member having a cam follower guiding contour extending along the cam member; a drive cam follower operatively connected to each power generating element. Each follower is adapted to engage the cam follower guiding contour throughout each reciprocation cycle of the power generating elements, the drive cam follower guiding contour following a generally sinusoidal profile on the surface of the drive cam member, the profile including a series of lobes forming peaks and troughs with intermediate regions therebetween, the peak to peak amplitude of the substantially sinusoidal profile of the cam follower guiding contour on the surface of the drive cam substantially corresponding to the stroke amplitude of the stroke of the reciprocating power generating elements. There are at least three drive cam followers spaced along the contour from one peak to an adjacent trough.
Abstract:
A Thermal actuation device has at least a heat expandable or deformable material, a heater, a power supply for the heating, a thruster capable of movement following expansion or distortion of a material, so as to perform a substantially predetermined stroke having a length from a first to a second position, at least an actuation element linearly following the action of the thruster so as to move with respect to a fixed structure from a first to a second position, and a resilient device able to return the thruster and/or actuation element respective first positions. A motion multiplyer actuated by the thrusting means is further provided for obtaining a stroke of the actuation element longer than the stroke of the thruster.
Abstract:
A cycle engine converting thermal energy to electricity includes a cylinder housing having a piston having two oppositely disposed heads and mounted for reciprocating inside the cylinder. The cylinder is disposed between a hot zone to supply hot gas to one piston head and a cold zone to receive discharged hot gas from another piston head, and to transform the discharged hot gas into a liquid. The hot zone supplies hot gas into the first piston head, while the second head discharges hot gas to the cold zone. This action creates a pressure differential between the two piston heads that causes the piston heads to move in one direction. Thereafter, the hot zone supplies hot gas to the second piston head, while the first piston head discharges hot gas to the cold zone, thereby creating pressure differential between the heads causing the piston to move in another direction. The piston is provided with a permanent magnet coupled to electric coil. When the piston reciprocates, it creates a magnetic influx in the electric coil, which is transformed into electricity in the coil.
Abstract:
A multi-dimensional, micro-electromechanical assembly and the method of fabricating same. The invention enables an assembly of three-dimensional (3D) microelectromechanical systems (MEMS) using surface tension or shrinkage self assembly. That is, the invention provides a surface tension self assembly technique for rotating a MEMS element with a controlled amount of deformation to a selected angle out of the plane of a substrate. In accordance with the inventive method, multi-dimensional, micro-electromechanical assemblies are fabricated by providing a phase change material on at least one substantially planar structure mounted in a first orientation. A phase change is induced in the phase change material whereby the phase change material changes from a first state, in which the structure is disposed in the first orientation, to a second state, in which the structure is disposed in a second orientation. The MEMS elements may be fabricated using conventional surface micromachining techniques. In the illustrative embodiment, each MEMS element is attached to a substrate by at least one hinge which allows rotation of the MEMS element out of the plane of the substrate to a selected angle. To enable mass assembly of the MEMS elements, the MEMS elements are rotated to the selected angle using either surface tension forces of a liquid phase change material or shrinkage of a solid phase change material. In the illustrative embodiment, the phase change material is solder and the step of inducing a phase change in the phase change material includes the step up applying heat.
Abstract:
Shape memory alloy actuators for aircraft landing gear are provided. In one embodiment a retractable aircraft landing gear system is provided. This embodiment includes a shape memory spring strut having a first end and a second end wherein the shape memory spring strut is extendable from a first length to a second length and the shape memory spring strut contains a shape memory alloy. This embodiment also includes a shape memory spring strut activation line connected to the shape memory spring strut wherein the shape memory spring strut activation line may be configured to activate the shape memory spring strut and a longitudinal connecting member having a first segment and a second segment wherein the first segment is in pivotal contact with the first end of the shape memory spring strut and the second segment supports a wheel rotatably mounted on a pin. The connecting member may be moveable along a line of travel from an extended position to a retracted position in this embodiment.
Abstract:
In a pulse tube refrigerator the refrigeration efficiency has been improved by reducing the on-off valve loss. A second space 47 in a cylinder member 41 is connected with a second high pressure on-off valve 23 and a second low pressure on-off valve 24. A buffer side on-off valve 25 is provided between the buffer space (a buffer tank 50) and the second space 47. By opening the buffer side on-off valve 25 before the second high pressure on-off valve 23 or the second low pressure on-off valve 24 is open, the pressure in the second space 47 can be the intermediate pressure. Since the pressure difference when the valves are open is decreased, the on-off valve loss can be decreased.
Abstract:
This invention provides stroke-multiplying shape memory alloy actuators and other actuators using electromechanically active materials nullcollectively referred to in this application as SMA actuatorsnull providing stroke multiplication without significant force reduction, that are readily miniaturizable and fast acting, and their design and use; economical and efficient control and sensing mechanisms for shape memory alloy actuators (including conventional shape memory alloy actuators as well as the stroke-multiplying SMA actuators of this invention) for low power consumption, resistance/obstacle/load sensing, and accurate positional control; and devices containing these actuators and control and sensing mechanisms.
Abstract:
A system and method for controlling a thermal dynamic cycle engine, such as a Stirling engine. The system includes a controller able to execute a program to alter certain aspects of the system to provide for a maximum power transfer and substantially stall free start up of the thermal dynamic cycle engine. Generally the controller is able to alter the current load to achieve a selected stroke length, pattern or temperature of a heater head of the engine. The system allows for generally stall free start-up and continuous control for maximum power (with maximum power factor) transfer from the thermal cycle engine or the associated alternator.